The aircraft is made from vacuum-molded composites with the design goal of strength at a light weight. Its 8.7 m (28.5 ft) span wing employs a Chris Mark 4 airfoil and mounts flaps. The standard engines available in 2012 were the 80 hp (60 kW) D-Motor LF26, the 100 hp (75 kW) Rotax 912ULS, the 100 hp (75 kW) Subaru EA 81 and the 116 hp (87 kW) Lycoming IO-233-LSAfour-stroke powerplants. By 2015 only the Subaru EA 81 and Rotax 912ULS were still offered. Floats for water operations are optional.[1][2][3][4][5]
Variants
Terrier 200
Base model with two molded individual seats.[1][2]
Terrier 200C
Model with bench seats that fold into a 200 by 105 cm (79 by 41 in) bed for camping.[1][2]
^ a b c d e fBayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 55. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
^ a b c d eTacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 56. Flying Pages Europe SARL, 2015. ISSN 1368-485X
^ a bFoxcon Aviation (n.d.). "Terrier 200". Retrieved 10 July 2012.
^Foxcon Aviation (n.d.). "Engine Choices". Archived from the original on 4 June 2012. Retrieved 5 January 2015.
^Foxcon Aviation (n.d.). "Powerplants". Retrieved 5 January 2015.
External links
Wikimedia Commons has media related to Foxcon Terrier 200.